MIT Libraries logoDSpace@MIT

MIT
View Item 
  • DSpace@MIT Home
  • Department of Aeronautics and Astronautics
  • Gas Turbine Laboratory
  • Gas Turbine Laboratory Reports
  • View Item
  • DSpace@MIT Home
  • Department of Aeronautics and Astronautics
  • Gas Turbine Laboratory
  • Gas Turbine Laboratory Reports
  • View Item
JavaScript is disabled for your browser. Some features of this site may not work without it.

Fluorescent visualization for turbomachine research

Author(s)
Epstein, Alan Harry
Thumbnail
Download04695809.pdf (1.852Mb)
Other Contributors
Massachusetts Institute of Technology. Gas Turbine Laboratory
Massachusetts Institute of Technology. Gas Turbine and Plasma Dynamics Laboratory
Metadata
Show full item record
Abstract
The quantitative gas fluorescence flow visualization technique using 2,3 butanedione as a tracer, has been refined and improved. Upgrading of the imaging system is responsible for the principal improvement. The technique has been applied to air flows in order to demonstrate its suitability to conventional compressor -testing. The possibility of using butanedione to measure static gas temperature has been explored by modeling. It has been found to be feasible only when a time lag after excitation of 1 ms is acceptable.
Description
March 1978
 
Includes bibliographical references (page 21)
 
Date issued
1978
URI
http://hdl.handle.net/1721.1/104416
Publisher
Cambridge, Mass. : Massachusetts Institute of Technology, Gas Turbine Laboratory, [1978]
Series/Report no.
GT & PDL report ; no. 142

Collections
  • Gas Turbine Laboratory Reports

Browse

All of DSpaceCommunities & CollectionsBy Issue DateAuthorsTitlesSubjectsThis CollectionBy Issue DateAuthorsTitlesSubjects

My Account

Login

Statistics

OA StatisticsStatistics by CountryStatistics by Department
MIT Libraries
PrivacyPermissionsAccessibilityContact us
MIT
Content created by the MIT Libraries, CC BY-NC unless otherwise noted. Notify us about copyright concerns.